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A midcourse guidance law for a solid-propellant rocket is proposed for exo-atmospheric interception based on an iterative predictor-corrector scheme.
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This page is a summary of: Composite Zero-Effort-Miss Guidance with Predictor–Corrector Steps for Ballistic Interception, Journal of Guidance Control and Dynamics, September 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007760.
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